N590AS
Service difficulty reports · 440
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N590AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N590AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2019061089654Display · inoperativeDISPLAY SOURCE 1 FAILURE LIGHT ILLUMINATED ON BOTH PFDS SPD LIM LIGHT ILLUMINATED CAPT PFD HYDRAULIC A PRESSURE DATA FIELD MISSING ENG LIGHT ILLUMINATED ON RECALL BUT EXTINGUISHED WHEN MASTER CAUTION LIGHT IS PRESSED. EEC BOTH REVERTED TO ALTN MODE. GROUNDED -SDR ASAA2019051329717Valve · out of limitsFOUND #2 ENGINE MAINT MSG 75-10592, THE TBV POSITION SIGNAL IS OUT OF RANGE. LONG TIME FAULT DEFERRED PER T/C 78273000. GROUNDED - YES. DEFERRED PER T/C 78273000. PLT DEFERRAL FOR 450 FLT HRS. ACCOMPLISHED B737-800 FIM 75-23 TASK 802. ACTUATORS TEST PASSES. FASDR ASAA201904295159Actuator · failedRIGHT HAND PACK LIGHT ON RECALL. RESETS WHEN PUSHING MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED RH RAM AIR ACTUATOR REF B737-800 AMM 21-51-21. OPS CHECK GOOD AT THIS TIME, BITE CHECK SHOWED NO FAULTS.SDR ASAA201904158956Actuator · leakingNR 1 ENGINE, LT VBV ACTUATOR LEAKING, APPROX 5 DROPS PER MINUTE, WHILE RUNNING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 VBV ACTUATOR IAW AMM 75-32-02. LEAK AND ACTUATORS TEST PASSED.SDR ASAA201904128965Fmc · failedL-FMC FAIL IN FLIGHT. UNABLE TO RESTORE W-QRH. GROUNDED - YES. RE-BOOTED LT FMC - OPS OK.SDR ASAA2019040538890Control Valve · failedON TAXI OUT, CONT CAB ZONE TEMP LIGHT DISPLAYED ON MASTER RECALL. RESET WITH MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED FLT DECK TRIM AIR MODULATING VALVE REF B737-800 AMM 21-61-21. 1 MIG-51A INSTL AND REMOVED OPS AND LEAK CK GOOD. PERFORMED CASDR ASAA2019033128838Valve · out of tolerance#2 ENGINE SHOWS FAULT CODE 75-10592- TBV POSITION SIGNAL IS OUT OF RANGE. LONG TIME FAULT REF T/C 78273000. GROUNDED - YES. REF B737-800 FIM 75-23 TASK 802. F/C 75-10592 ACTIVE. TBV DATA SHOWS DEMAND AT 100%. POSITION AT 6%. FADEC 3 S/W. PERFORMED GVI OF J9/J1SDR ASAA2019030528496Warning System · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL EXTINGUISHED WITH MC RESET. GROUNDED - YES. PERFORMED PACK/ZONETEMP CONT BITE TEST PER AMM 21-61-00 SYSTEM CHECKS GOOD.SDR ASAA2019030128462Actuator · defectiveWHILE PERFORMING T/C #7827300 FOUND LONG TIME FAULT MESSAGE #75-20391 "THE VSV POSITION SIGNAL IS OUT OF RANGE." DEFERRED PER T/C #78273000 ON NR 1 ENG. GROUNDED - YES. REMOVED AND REPLACED THE NR 1 ENG LT VSV ACTUATOR, LEAK CHECK GOOD. ACTUATOR TEST PASS AND SDR ASAA2019022748353Actuator · failedR/H PACK LIGHT ILLUMINATES ON RECALL AND RESETS WHEN MASTER CAUTION IS PUSHED. GROUNDED - YES. BITE TEST ON #2 CONTROLLER SHOWS ACTUATOR FAILURE. FAULT WILL NOT RESET. REMOVED AND REPLACED RAM AIR ACTUATOR #2 IAW B737-800 AMM 21-51-21. PERFORMED #2 PACK/ZONE TSDR ASAA2019020328683Eec · failedWHILE PERFORMING T/C 78273000 FOUND ECONOMIC FAULT CODE 75-10542 THE LPTACC POSITION SIGNAL IS OUT OF RANGE, DEFERRED PER T/C 78273000. GROUNDED - YES. DEFERRED PER T/C 78273000 FOR 500 FLT HRS. REPLACED NR 2 ENG EEC PER AMM 73-21-00-700-802-F00. FADEC SYS TESSDR ASAA2019012927974Fmc · malfunctionedON TAXI IN WE HAD A DUAL FMC FAILURE (VTK ON BOTH NAV DISPLAYS). ABOUT 30 SECONDS LATER THE PROBLEM CLEARED AND OPS NORMAL. GROUNDED - YES. PERFORMED FIM 34-61 TASK 801, NO FAULTS LOGGED. PERFORMED FIM 34-61 TASK 807 AND FOUND 1 FAULT (FMC-L PGM FAULT). LT ANDSDR ASAA2019011927869Lens · detachedEXIT SIGN BY L1 DOOR HINGE CAME UNDONE. GROUNDED - YES. REINSTALLED EXIT SIGN LENS AS REQUIRED.SDR ASAA2019011427795Modulating Valve · failedAFTER START, RIGHT HAND PACK LIGHT ILLUMINATED ON RECALL. LIGHT EXTINGUISHED ON RESET. GROUNDED - YES. REPLACED RIGHT PACK TCV (V141) INSTALLATION TEST PASSES, NO LEAKS NOTED. REF AMM 21-51-10-400-801. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019011227801Not Reported · malfunctionedWHILE PERFORMING TASK CARD, FOUND NR 1 ENGINE FAULT 75-20391, LONG TIME FAULT. THE VSV POSITION SIGNAL IS OUT OF RANGE. GROUNDED - YES. APPLIED LONG TIME FAULT DEFERRAL 450 FLT HRS. MSG 75-20391 ON NR 1 ENGINE DEFERRED PER T/C 78273000. FAULT CODE 75-20391 ON SDR ASAA2018120927363Wire Harness · defectiveWHILE PERFORMING TASK CARD FOUND NR 1 ENGINE FAULT 75-20391, LONG TIME FAULT. THE VSV POSITION SIGNAL IS OUT OF RANGE. GROUNDED - YES. ON DEFERRAL. ACCOMPLISHED FIM 75-34 TASK 819. FOUND J6 (CH B) WIRE HARNESS RESISTANCE NOT IN SPECIFIED RANGE. REMOVED AND RESDR ASAA2018111956875Starter · inoperativeFLT CREW REPORTS #1 ENGINE WILL NOT START, START VALVE LIGHT ILLUMINATES WITH NO N1 OR N2 ROTATION. GROUNDED - YES. PERFORMED #1 ENG STARTER OVERRIDE, NO N1 NOR N2 ROTATION. SUSPECT BAD STARTER. REMOVED AND REPLACED #1 ENG STARTER PER B737-800 AMM 80-11-01. OPSDR ASAA2018111396802Filter · dirtyGOT A "CONT CAB" ZONE TEMP LIGHT APPLIED QRH - COOLED THE FLIGHT DECK AND LIGHT EXTINGUISHED. SAME SITUATION OCCURRED A SECOND TIME. GROUNDED - YES. PERFORMED INITIAL EVALUATION FOR FLT DECK ZONE TRIM VALVE FAULT PER B737-800 FIM 21-62 TASK 832 AND TASK 833 - SDR ASAA2018110826825Pin · missingWHILE ACCOMPLISHING TC SBCFM56-7B-72-0986-1 INSP OF METALLIC HYBRID VSV SYS FOUND HPC STG 3 VSV PIN MISSING AT 3 OCLOCK POSITION WITH FOD DAMAGE BEYOND AMM 72-00-00-200-804-F00 STAGE 3 & STAGE 4, WITH NICKS ON ROTOR SHAFT DUE TO LIBERATION OF PIN. MIG 2C 40-00SDR ASAA2018110426907Receptacle · corrodedNR 1 ENGINE FAULTS DISCOVERED DURING EEC BITE TEST. MSG 75-20391 LONG TIME FAULTS. THE VSV POSITION SIGNAL IS OUT OF RANGE. GROUNDED - YES. FAULT 75-20391 LOGGED ON FLIGHT 3 LEG IN FAULT HISTORY. ACCOMPLISHED FIM 75-31 TASK 803, VERIFIED SPLIT BETWEEN CHAN A &SDR ASAA2018110426738Fault Code · displayed# 1 ENGINE FAULTS DISCOVERED DURING EEC BITE TEST. MSG 75-20391 LONG TIME FAULTS. THE VSV POSITION SIGNAL IS OUT OF RANGE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018102226583Bolt · wornNR 2 ENGINE FAN FRAME OUTBOARD STRUT COVER HAS A FASTENER HEAD WORN BOTTOM SIDE. GROUNDED - YES. REPLACED DAMAGE FASTENER SEE MIG 2C 40-0026341 FOR DETAILS.SDR ASAA2018101226481Fcu · faultyAPU COLD SOAKED START ATTEMPT FAILED AT 360 APU FAULT LIGHT APPEARED. GROUNDED - YES. ACCOMPLISHED APU BITE PROCEDURE REF FIM 49-60 TASK 801, LOGGED FAULT 49-31016 OVER TEMPERATURE SHUTDOWN. ACCOMPLISHED FIM 49-30 TASK 803 OVER TEMPERATURE SHUTDOWN- FAULT ISOLSDR ASAA2018101026451Fmc · malfunctionedBEFORE TAXI OUT IN EWR PERF DATA CAME UP MULTIPLE TIMES ON BOTH CDU DISPLAYS WITH EXACT SAME DATA BUT REQUIRING PILOTS TO ACTIVATE MULTIPLE TIMES LATER IN FLIGHT SAME OCCURRENCE FOR PERF INIT ENTRIES WIND ENTRIES ETC., BOTH FMC'S SEEM TO FUNCTION & PROCESS NOTSDR ASAA2018100626413Sensor · failedFAULT LIGHT ILLUMINATED ON APU CSS AT FL380. GROUNDED - YES. CHECKED MAG PLUG PER FIM 49-60 TASK 817 STEP 4. NO DEFECTS NOTED. REPLACED SPEED SENSOR PER FIM 49-60 TASK 817 STEP 8 AND AMM 49-61-21. OPS CK GOOD, LK CK GOOD. NO FAULTS FOUND. STARTED APU SEVERAL TSDR ASAA2018092876297Connector · looseL2 DOOR OVER DOOR EMERGENCY EXIT SIGN AND EMERGENCY EXIT LOCATOR SIGN WILL NOT ILLUMINATE. GROUNDED - YES. FOUND CONNECTOR D40044P LOOSE RECONNECTED CONNECTOR. OPS CHECKD PER B737-800 AMM 33-51-00. OPS CHECKED GOOD.SDR ASAA2018091726151Warning System · false activationWHILE PERFORMING T/C 78273000 FOUND NR 1 ENGINE HAS "THE VSV POSITION SIGNAL IS OUT OF RANGE" LONG TIME FAULT 75-20391. GROUNDED - YES. PERFORMED EEC BITE IAW FIM 73-00 TASK 801. FOUND NO FAULTS. PERFORMED ACTUATORS TEST IAW AMM 71-00-00-700-807-F00. GROUND VESDR ASAA201808205811Controller · failedAUTO FAIL LIGHT ILLUMINATED. ACFT GROUNDED. REPLACED THE NR 1 CABINE PRESSURE CONTROLLER IAW AMM 21-31-01. ACCOMPLISHED PRESSURIZATION SYSTEM GROUND TEST IAW AMM 21-31-00. SYSTEM TEST PASSED. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2018081645795Warning Light · false activationMASTER CAUTION ILLUMINATED ON LANDING ROLL. AUTO FAIL ON PRESSURIZATION PANEL AND ALTN LIGHT REMAINED ILLUMINATED ON OVERHEAD. ACFT GROUNDED. CYCLED CABIN PRESSURE CONTROLLER CIRCUIT BREAKERS IAW AMM 20-60-05, OPS CHECKED NORMAL, PERFORMED BITE CHECK BOTH DSDR ASAA2018081545787Release Mech · brokenF/A REPORTED THE R1 DOOR GIRT BAR STOP ASSY, RELEASE WAS BROKEN. ACFT GROUNDED. REPLACED THE GIRT BAR STOP ASSY RELEASE IAW AMM 25-66-01-000-804.SDR ASAA2018080765687Warning Light · false indicationPRESSURIZATION PANEL, AUTO FAIL LIGHT ALONG WITH ALTERNATE LIGHT ILLUMINATED AT 500 AGL. LANDED. ACFT GROUNDED. IAW FIM 21-31, TASK 827. PERFORMED INITIAL EVALUATION AUTO FAIL LIGHT EXTINGUISHED FAULT HAS BEEN CORRECTED AND CONTROLLER IS OPERATING NORMALLSDR ASAA2018080125608Warning System · false activationPRESSURIZATION CONTROL PANEL "AUTO FAIL" LIGHT ILLUMINATED ON SHORT FINAL APPROACH. GROUNDED - YES. VERIFIED DISCREPANCY. FOUND NR 1 CONTROLLER FAULTING LRU CODE 57. PERFORMED FIM 21-31 TASK 801 (DCPC) BITE PROCEDURE. NO ACTIVE FAULTS FOUND. SYS RESET. FAULT CSDR ASAA2018073025545Controller · malfunctionedPRESSURE CONTROLLER SHOWED AUTO FAIL QRH FOLLOWED. GROUNDED - YES. CYCLED PRESSURE CONTROLLER SELECTOR FROM AUTO TO MANUAL & FAULT CLEARED. RAN PRESSURE CONTROLLER 1 & 2 BITE PER AMM 21-31-00 - NO FAULTS NOTED.SDR ASAA2018062025156Warning Light · false activationAUTO FAIL AND ALTN LIGHTS ILLUMINATED ON PRESSURIZATION PANEL. GROUNDED - YES. RESET AUTO FAIL LT REF FIM TASK 21-31-TASK 827 -LIGHTS RESET OK. BITE TEST OF DIGITAL CABIN PRESS CONTROLLER OK REF. FIM TASK 21-31 TASK 801 ETOPS GROUND VERIFICATION COMPLETE.SDR ASAA2018061164983Bulkhead Web · crackedPRESSURE BULKHEAD WEB AT BS 663 WAS CRACKED IN THE MACHINED POCKET BETWEEN RBL 37 AND RBL 45. ACFT GROUNDED. REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10-2R-3.SDR ASAA2018051624957Lug · corrodedLEFT HORIZONTAL STAB AFT ATTACH FITTING, LOWER LUG STAB SIDE, AFT SIDE HAS EVIDENCE OF CORROSION. ACFT GROUNDED. REPAIRED THE ATTACH FITTING LOWER LUG IAW EA EA 20332.SDR ASAA2018060424878Support Angle · crackedFWD CARGO BAY, LBL 25 AND RBL 25 SUPPORT ANGLE WAS CRACKED AT BS 500H, FWD SIDE OF FRAME. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0.SDR ASAA2018060424876Support Angle · crackedFWD CARGO BAY, LBL 25 INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500G, FWD SIDE OF FRAME. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0.SDR ASAA2018051125023Battery Pack · failedEMERGENCY BATTERY PACK M1675 AT STATION 322 FAILED DEEP CYCLE CHECK. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK S/N 80643 M1675 AND OPS CHECKED GOOD IAW AMM 33 51 06 960 805 STEPS 4D 1-5.SDR ASAA2018051125022Battery Pack · dischargedLEFT AFT OVERWING HATCH, OUTSIDE EMERGENCY EXIT LIGHT INOP. GROUNDED - YES. RELAMPED LT AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33 51 04 960 801, AND REPLACED BATTERY PACK S/N 87698 FOR LT AFT EMERGENCY LIGHT IAW AMM 33 51 06 960 805, OPS CKS GOOD IAW AMM 33SDR ASAA2018051124984Battery Pack · no testEMERGENCY BATTERY PACK M1671 AT BS 727C+13 FAILED A DEEP CYCLE TEST. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-06-960-805, STEPS 4.D 1 - 5.SDR ASAA2018040924199Fmc · failedBOTH FMC P/RST LIGHTS ILLUMINATED WITH NO MESSAGE ON THE SCRATCH PAD. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 FMC IAW AMM 34-61-02-07-01. PERFORMED A SOFTWARE VERIFICATION IAW AMM 34-61-00/201. VERIFIED FMCS PERFORMANCE FACTORS ADJUSTMENTS IAW AMM 34-61SDR ASAA2018040824161Fmc · failedLEFT FMC FAILED. ACFT GROUNDED. REMOVED AND REPLACED LEFT FMC COMPUTER, ALL INSTALLATION TESTS PASSED IAW AMM 34-61-02.SDR ASAA2018040624163Igniter · failedAPU FAULT LIGHT ILLUMINATED DURING ATTEMPTED START. ACFT GROUNDED, BITE CHECK OF APU REPORTED ONE HISTORY FAULT, 49-41011. NO FLAME SHUT DOWN, AND ONE CURRENT FAULT, 49-31168 FUEL CONTROL UNIT SHOWS OUT OF RANGE HIGH. REMOVED AND REPLACED APU IGNITION UNITSDR ASAA2018032824058Warning Message · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL, EXTINGUISHED ON RESET. ACFT GROUNDED. INDICATED RT PACK LIGHT BUT LT PACK CONTROLLER WAS DEFERRED. PERFORMED PACK/ZONE TEMPERATURE CONTROLLER BITE TEST ON BOTH THE LT & RT CONTROLLERS IAW AMM 21-61-00-700-806-002. NRSDR ASAA2018022823724Probe · failedTEMP PROBE LIGHT ILLUMINATED IN FLIGHT, CIRCUIT BREAKER IS STILL IN. ACFT GROUNDED. REMOVED AND REPLACED THE TAT PROBE IAW AMM 34-21-06. GROUND TESTED OK IAW AMM 30-31-00-730-801.SDR ASAA2018022123652Control Valve · faultedRIGHT PACK LIGHT ON RECALL, RESETS WHEN PRESSING MASTER CAUTION. ACFT GROUNDED. PERFORMED A RIGHT PACK TEMPERATURE CONTROL BITE IAW FIM 21-62 TASK 801, RIGHT TCV LIGHT ILLUMINATED ON CONTROLLER. REMOVED AND REPLACED THE RT TEMP CONTROL VALVE V141 IAW AMSDR ASAA2018022023658Knob · failedCAPTAIN`S FMC BRIGHTNESS DOES NOT HAVE DIM TO BRIGHT STOPS. KNOB TURNS THRU DIM TO BRIGHT TO DIM. ACFT GROUNDED. REMOVED AND REPLACED MCDU IAW AMM 34-61-01, GROUND VERIFICATION TEST PASSED.SDR ASAA2018022023650Warning Light · false activationRIGHT PACK LIGHT COMES ON WITH MASTER CAUTION RECALL, LIGHT GOES OUT WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED A PACK-ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-61-00, RESET SYSTEM, SYSTEM OP CHECKED GOOD, NO HISTORY LAST 60 DAYS.SDR ASAA2018012823319Warning Message · false activationMASTER CAUTION OVERHEAD & PACK LIGHTS ILLUMINATED. RESET MASTER CAUTION AND ALL CAUTION LIGHTS EXTINGUISHED. ACFT GROUNDED. THE NR 1 PACK/TEMP CONTROLLER SHOWS RAM AIR ACTUATOR FAULT ON BIT TEST. PREV FLT & VERIFY PASSED. RESET FAULT. FAULT DID NOT RETURN.
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